# N934FD: 1988 Boeing 757-21B

- Status: Valid registration
- Airframe: [Boeing 757-21B](https://openairdocs.org/model/boeing-757-21b) (registry code 1384917, 239 seats)
- Engine: [Rolls-Royce RB211-535E4 series](https://openairdocs.org/engine/rolls-royce-rb211-535e4-series) (registry code 54223)
- Data sheets: [TCDS E12EU](https://openairdocs.org/tcds/E12EU) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 24331
- Year built: 1988
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 7, 2009
- Certificate issued: September 12, 2008
- Expires: May 31, 2028
- Mode S code: ACF506
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=934FD
- Page: https://openairdocs.org/aircraft/N934FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce RB211-535E4 model are included.

## ADs that may apply (OpenAirDocs): 20 in force

### Matched by airframe (Boeing 757-21B)

None in force.

### Matched by engine (Rolls-Royce RB211-535E4 series)

- [AD 2024-10-06](https://openairdocs.org/ad/2024-10-06): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jun 27, 2024
- [AD 2020-08-03](https://openairdocs.org/ad/2020-08-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective May 18, 2020
- [AD 2017-24-08](https://openairdocs.org/ad/2017-24-08): Fuel control/Turbine engines · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 16, 2018
- [AD 2016-03-04](https://openairdocs.org/ad/2016-03-04): Life-limited rotating parts · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Mar 15, 2016
- [AD 2013-23-17](https://openairdocs.org/ad/2013-23-17): High-pressure (HP) and intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-C-37 and 3 more. Effective Dec 11, 2013
- [AD 2013-16-23](https://openairdocs.org/ad/2013-16-23): Cracked and distorted FCL metering panel · Rolls-Royce RB211-524B-02, RB211-524B2-19, RB211-524B3-02 and 13 more. Effective Oct 8, 2013
- [AD 2012-25-09](https://openairdocs.org/ad/2012-25-09): Intermediate-pressure (IP) turbine discs · Rolls-Royce RB211-524G2-19, RB211-524G2-T-19, RB211-524G3-19 and 10 more. Effective Feb 6, 2013
- [AD 2012-02-11](https://openairdocs.org/ad/2012-02-11): LP turbine stage 1, 2, and 3 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Mar 6, 2012
- [AD 2009-20-14](https://openairdocs.org/ad/2009-20-14): Eddy current inspection (ECI) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Nov 17, 2009
- [AD 2008-20-04](https://openairdocs.org/ad/2008-20-04): HP turbine discs · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 26 more. Effective Nov 3, 2008
- [AD 2006-11-05 R2](https://openairdocs.org/ad/2006-11-05-R2): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 21, 2008
- [AD 2007-14-07](https://openairdocs.org/ad/2007-14-07): Fluorescent penetrant inspections (FPI) · Rolls-Royce RB211-524B-02, RB211-524B-B-02, RB211-524B2-19 and 21 more. Effective Aug 16, 2007
- [AD 2006-17-12](https://openairdocs.org/ad/2006-17-12): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Sep 27, 2006
- [AD 2004-19-04](https://openairdocs.org/ad/2004-19-04): Critical Life-Limited Rotating Engine Parts · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Nov 1, 2004
- [AD 2004-01-21](https://openairdocs.org/ad/2004-01-21): Frount engine mount housing · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 27, 2004
- [AD 2003-10-03 R1](https://openairdocs.org/ad/2003-10-03-R1): High pressure (HP) turbine discs · Rolls-Royce RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2001-19-05](https://openairdocs.org/ad/2001-19-05): High Speed Gearbox Drive · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Oct 11, 2001
- [AD 2000-09-14](https://openairdocs.org/ad/2000-09-14): Radial Drive Steady Bearings · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Jul 11, 2000
- [AD 97-02-12](https://openairdocs.org/ad/97-02-12): Fuel Flow Governor (FFG) · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 4, 1997
- [AD 87-25-04](https://openairdocs.org/ad/87-25-04): Fuel Quantity Indication System · Rolls-Royce RB211-535C-37, RB211-535E4-37, RB211-535E4-B-37 and 1 more. Effective Dec 8, 1987

### Historical (superseded or no longer in force)

- [AD 2015-17-21](https://openairdocs.org/ad/2015-17-21) (historical): High-pressure turbine (HPT) disks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Dec 2, 2015
- [AD 2014-24-08](https://openairdocs.org/ad/2014-24-08) (historical): Fuel leaks · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-C-37. Effective Jan 6, 2015
- [AD 2013-19-18](https://openairdocs.org/ad/2013-19-18) (historical): LPT stage 2 disc failure · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Nov 7, 2013
- [AD 2013-19-17](https://openairdocs.org/ad/2013-19-17) (historical): Failure of rotating life limited parts · Rolls-Royce RB211-535E4-B-37. Effective Nov 7, 2013
- [AD 2011-11-08](https://openairdocs.org/ad/2011-11-08) (historical): LP Turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37, RB211-535E4-B-75 and 1 more. Effective Jun 30, 2011
- [AD 2008-22-24](https://openairdocs.org/ad/2008-22-24) (historical): Low pressure compressor (LPC) fan blade · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 9, 2008
- [AD 2006-11-05 R1](https://openairdocs.org/ad/2006-11-05-R1) (historical): Disc assemblies · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective May 1, 2007
- [AD 2006-11-05](https://openairdocs.org/ad/2006-11-05) (historical): High pressure compressor (HPC) stage 3 disc assemblies · Rolls-Royce RB211-22B-02, RB211-524B-02, RB211-524B-B-02 and 24 more. Effective Jun 27, 2006
- [AD 2005-02-05](https://openairdocs.org/ad/2005-02-05) (historical): Low Pressure Compressor (LPC) Fan Blade Roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Feb 11, 2005
- [AD 2004-26-03](https://openairdocs.org/ad/2004-26-03) (historical): High pressure (HP) turbine discs · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 3 more. Effective Jan 13, 2005
- [AD 2004-01-20](https://openairdocs.org/ad/2004-01-20) (historical): High pressure compressor (HPC) · Rolls-Royce RB211-22B-02, RB211-22B/MOD 72-8700, RB211-524B-02 and 27 more. Effective Feb 24, 2004
- [AD 2003-17-15](https://openairdocs.org/ad/2003-17-15) (historical): Low pressure (LP) turbine stage 2 discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Oct 2, 2003
- [AD 2003-12-15](https://openairdocs.org/ad/2003-12-15) (historical): LPC fan blade roots · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jul 30, 2003
- [AD 2003-10-03](https://openairdocs.org/ad/2003-10-03) (historical): High Pressure (HP) turbine discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Jun 20, 2003
- [AD 2002-23-08](https://openairdocs.org/ad/2002-23-08) (historical): Low Pressure (LP) Turbine Stage 2 Discs · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Dec 30, 2002
- [AD 2001-23-02](https://openairdocs.org/ad/2001-23-02) (historical): High Pressure Turbine Disks · Rolls-Royce RB211-22B-02, RB211-535C-37, RB211-535E4-37 and 2 more. Effective Dec 24, 2001
- [AD 98-07-07](https://openairdocs.org/ad/98-07-07) (historical): Fuel System Tube Assembly · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective Apr 29, 1998
- [AD 86-07-01](https://openairdocs.org/ad/86-07-01) (historical): Outer Combustion Case Inspection · Rolls-Royce RB211-535E4-37, RB211-535E4-B-37 and RB211-535E4-B-75. Effective May 16, 1986

## Information bulletins (advisory) (1 in force)

- [SAIB 2026-11](https://openairdocs.org/saib/2026-11): Theft of Turbofan Engine Parts before Mutilation. Issued Jun 8, 2026

## NTSB investigations

None matched to N934FD.

## FAA accident and incident reports

None matched to N934FD.

## Service difficulty reports (539, newest 50)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR FDEA202609091291](https://openairdocs.org/sdr/FDEA202609091291), Sep 9, 2026: FLAP SYSTEM. FAULTED. TE FLAP DISAGREE WHEN GOING FROM FLAPS 20 TO 25. RAN QRH. DECLARED EMERGENCY ***EMERGENCY DECLARED*** CARRIED OUT FIM TASK 27-51 808 ON TRAILING EDGE FLAP SYSTE
- [SDR FDEA202608201185](https://openairdocs.org/sdr/FDEA202608201185), Aug 20, 2026: ENGINE. DAMAGED. ON CLIMB AT ABOUT 18000 FT RIGHT ENGINE EGT WENT INTO YELLOW RANGE. ENTERED HOLDING TO RUN ENGINE LIMIT OR SURGE OR STALL QRH. ENGINE WAS UNRESPONSIVE TO POWER 
- [SDR FDEA202606160765](https://openairdocs.org/sdr/FDEA202606160765), Jun 16, 2026: NOT REPORTED. NOT REPORTED. WRI 57-40-5108 FACTED IN ERROR. EA: F-5740-T0387288 P1. CREATED WRI 5740-5115 FOR SDR OF WRI 5740-5108 BEING FACTED IN ERROR. REF MAJOR REPAIR E.A. F-5740-T0387
- [SDR FDEA202601280090](https://openairdocs.org/sdr/FDEA202601280090), Jan 28, 2026: BATTERY. FAILED. ON SERVICE CHECK, NOTED CENTER GALLEY EXIT SIGN & R1 DOOR EXIT SIGN, & R1 DOOR SLIDE LIGHT NOT ILLUMINATING ON TEST. R & R FWD GALLEY EMERGENCY LIGHT POWER SUPP
- [SDR FDEA202506271069](https://openairdocs.org/sdr/FDEA202506271069), Jun 27, 2025: STRINGER. CORRODED. DOT 80-059 AFT CARGO COMPARTMENT STR 27R/H JUST AFT OF F/S 1300 @ DOME NUT STRINGER EXFOLIATED. CORROSION FOUND TO BE OUT LIMITS IAW SRM 53-00-03 FIG 101 ACCOMP
- [SDR FDEA202506271068](https://openairdocs.org/sdr/FDEA202506271068), Jun 27, 2025: STRAP. CORRODED. DOT 86-117 AFT CARGO STA 1420, STABILIZER STRAP IN CEILING AT RBL 45, CORRODED. REMOVED STABILIZER STRAP IN CEILING AT RBL 45 AND PEFORMED REPAIR IAW SRM 53-00-
- [SDR FDEA202506251047](https://openairdocs.org/sdr/FDEA202506251047), Jun 25, 2025: SKIN. CORRODED. DOT 86-84 RH WING IB MAIN FLAP, CORROSION ON UPPER SURFACE EDGE, AT OB JUNCTION OF AFT FLAP. REMOVED, REPAIRED AND REINSTALLED RH WING MAIN FLAP UPPER SURFACE E
- [SDR FDEA202506241038](https://openairdocs.org/sdr/FDEA202506241038), Jun 24, 2025: SEAT TRACK. CORRODED. UNDER CABIN FLOOR PNL. 242MAF, AROUND MANY SCREWHOLES HAVE SURFACE CORROSION, ON FLOOR STRUCTURE. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW SRM 53-00-51-
- [SDR FDEA202506211022](https://openairdocs.org/sdr/FDEA202506211022), Jun 21, 2025: FLOOR PANEL. BROKEN. AFT CABIN FLOOR PANEL 251 MWF IS BROKEN AND MISSING CORRECT INSERT. FABRICATED MAIN CABIN FLOOR PANEL 251 MWF ON VTMAE TRAVELER T25/1818647 PER DWG 11864182, MA
- [SDR FDEA202506211021](https://openairdocs.org/sdr/FDEA202506211021), Jun 21, 2025: FLOOR PANEL. DAMAGED. MAIN CABIN FLOOR PANEL 252 MWF IS BROKEN AND HAS ALL WRONG INSERTS NOT FLUSH WITH THE PANEL ARE INSTALLED ALL THE WAY THROUGH THE PANEL, NEEDS THE VERY SHALLOW 
- [SDR FDEA202506211020](https://openairdocs.org/sdr/FDEA202506211020), Jun 21, 2025: FLOORBOARD. DAMAGED. MAIN CABIN FLOORBOARD 251MVF IS BROKEN. FABRICATED MAIN CABIN FLOORBOARD 251MVF ON VTMAE TRAVELER T25/1818699 PER DWG 11864182, MAJOR REPAIR.
- [SDR FDEA202506191011](https://openairdocs.org/sdr/FDEA202506191011), Jun 19, 2025: SEAT TRACK. CORRODED. CORR. FOUND ON SEAT TRACK LBL 45 FROM 1180 TO 1280 REMOVED, FABRICATED NEW & INSTALLED MAIN CABIN SEAT TRACK FROM STA 1180-1280 LBL 45 PER DWG BAC 1520-792 & SR
- [SDR FDEA202506191008](https://openairdocs.org/sdr/FDEA202506191008), Jun 19, 2025: STRAP. DAMAGED. BROKEN FLANGE STRAP UNDER CABIN FLOOR PNL #222 MDF B STA 396 DOT# 204-16 REMOVED & REPLACED STRAP UNDER FLOOR PANEL #222 MDF AT STA 396 IAW SRM 53-10-51-2R- 1, 
- [SDR FDEA202506191007](https://openairdocs.org/sdr/FDEA202506191007), Jun 19, 2025: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK AT STA 1189 RBL 58.2 HAS CORROSION AT FASTENER HOLES. DOT 4-142 REMOVED AND REPLACED NEW SEAT TRACK PER DWG BAC1520-792, BATCH #0004393834
- [SDR FDEA202506191006](https://openairdocs.org/sdr/FDEA202506191006), Jun 19, 2025: CROSSBEAM. CORRODED. DOT 86-160 STA 1060-1100, LBL 0-24 CORROSION AROUND SCREWHOLES. CROSSBEAM AT BS 1060-1100, BL0-LBL24 CORROSION BEYOND ALLOWABLE LIMITS, REMOVED DAMAGE CROSSBEAM
- [SDR FDEA202506130929](https://openairdocs.org/sdr/FDEA202506130929), Jun 13, 2025: SEAT TRACK. CORRODED. DOT 86-158 FLOOR TRACK AT LBL24, STA 1057, CORROSION ON LH FLANGE AT SCREWHOLE. REMOVED AND REPLACED FLOOR TRACK AT LBL 24 STA 1057 IAW SRM 51-40-02 & DWG 111N5
- [SDR FDEA202506110921](https://openairdocs.org/sdr/FDEA202506110921), Jun 11, 2025: REPAIR. CORRODED. DOT 80-065 AFT CARGO COMPARTMENT CEILING STRUCTURE. FLOOR BEAM LOWER FLANGE. F/S 1560 APPROX 10 INCHES FROM R/H SIDEWALL BEAM CORRODED REMOVED DAMAGES AT AFT CA
- [SDR FDEA202506100886](https://openairdocs.org/sdr/FDEA202506100886), Jun 10, 2025: STRAP. CORRODED. DOT 86-118 AFT CARGO STA 1420, STABILIZER STRAP IN CEILING AT RBL 24, CRRODED. REMOVED AND REPLACED STABILIZER IN CEILING STRAP IAW SRM 51-40-02, FABRICATED ON 
- [SDR FDEA202506100885](https://openairdocs.org/sdr/FDEA202506100885), Jun 10, 2025: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK HAS CORROSION A STA 1180 TO 1200 RBL 45, DOT 4-141 REMOVED, FABRICATED & INSTALLED NEW MAIN CABIN SEAT TRACK PER DWG BAC 1520-792 STA 1120
- [SDR FDEA202501080035](https://openairdocs.org/sdr/FDEA202501080035), Jan 8, 2025: BULB. INOPERATIVE. SLIDE LIGHT WOULD NOT ILLUMINATE WHEN RIGHT ENTRY DOOR WAS ARMED. REPLACED R1 DOOR SLIDE LIGHT BULBS, READY FOR SERVICE.
- [SDR FDEA202401160079](https://openairdocs.org/sdr/FDEA202401160079), Jan 16, 2024: PROBE. FAILED. DURING CLIMB OUT AFTER TURNING OFF ENGINE ANTI-ICE THE LEFT ENGINE APPEARED TO NOT PRODUCE THE SAME POWER AS THE RIGHT ENGINE. 7 DEGREES RIGHT RUDDER REQUIRED. 
- [SDR FDEA202309081563](https://openairdocs.org/sdr/FDEA202309081563), Sep 8, 2023: POWER SUPPLY. FAILED. L1 DOOR EMERGENCY LIGHT ABOVE DOOR AND SLIDE LIGHT FAILED TO ILLUMINATE DURING TEST. REMOVED AND REPLACED L1 DOOR POWER SUPPLY AS REQUIRED OPS CKS NORMAL OK FOR
- [SDR FDEA202307181233](https://openairdocs.org/sdr/FDEA202307181233), Jul 18, 2023: CYLINDER. FAILED. L FWD ENT DOOR ARMED FLAG DID NOT FUNCTION. UPON OPENING DOOR THE SLIDE PARTIALLY DEPLOYED. FOUND L1 DOOR OPEN WITH SLIDE HANGING OUT OF DOOR AND ATTACHED TO GI
- [SDR FDEA202306301130](https://openairdocs.org/sdr/FDEA202306301130), Jun 30, 2023: UNKNOWN. CORRODED. MAIN CABIN - SEAT TRACK AT STA565 TO 575 LBL24 HAS CORROSION BY FLOOR PANELS HOLES CORROSION ON MAIN SEAT STA 565 TO STA 575 LBL 24 FOUND TO BE OUT OF LIMITS IA
- [SDR FDEA202306281124](https://openairdocs.org/sdr/FDEA202306281124), Jun 28, 2023: SKIN. WORN. L.WING O/B FWD FLAP I/B L/E REINFORCING DOUBLER IS WORN. REPAIRED L/E SKIN ON L.WING O/B MAIN FLAP PER B757 SRM 57-53-01-2R, REPAIR 5
- [SDR FDEA202306261109](https://openairdocs.org/sdr/FDEA202306261109), Jun 26, 2023: ATTACH ANGLE. CORRODED. L.WING L/E #3 SLAT IS CORRODED ON THE LOWER ATTACH ANGLE FOR COVE SKIN.. REMOVED AND REPLACE #3 SLAT ASSY ON FEDEX N/R N00374 AND HAECO N/R 22374. PER B757 AMM 
- [SDR FDEA202306241092](https://openairdocs.org/sdr/FDEA202306241092), Jun 24, 2023: SLAT. DENTED. LH WING #5 SLAT LOWER SURFACE OF T/E WEDGE IS DENTED JUST O/B OF I/B AUX TRACK REPAIRED LH WING #5 SLAT LOWER SKIN BY REMOVING DAMAGE AREA AND BONDING FILLER AN
- [SDR FDEA202306211070](https://openairdocs.org/sdr/FDEA202306211070), Jun 21, 2023: PANEL. CRACKED. LEFT WING FIXED LEADING EDGE SKIN UPPER SURFACE CRACKED IN TWO EACH AREAS AT INBD END OF #3 SLAT. REPAIRED L/H WING FIXED LEADING EDGE SKIN UPPER SURFACE IS CRA
- [SDR FDEA202306181055](https://openairdocs.org/sdr/FDEA202306181055), Jun 18, 2023: SLAT. DENTED. LH #5 SLAT, INNER SKIN IS DENTED JUST OUTBD OF INBD AUX TRACK. REPAIRED L/W #5 SLAT COVE PANEL SKIN DENTED AND PUNCTURED IAW B757 SRM 57-43-01-2R REPAIR 3
- [SDR FDEA202306171045](https://openairdocs.org/sdr/FDEA202306171045), Jun 17, 2023: SKIN. BURNED. EXTERIOR FUSELAGE SKIN HAS LIGHTNING STRIKE DAMAGE AT STA 1547 BETWEEN S23R & S24R EVALUATED LIGHTNING STRIKE @ STA 1547 BETWEEN S23R & S24R MATL LOSS .010 MATL
- [SDR FDEA202306141035](https://openairdocs.org/sdr/FDEA202306141035), Jun 14, 2023: FLAP. DELAMINATED. RIGHT WING I/B FWD FLAP I/B END UPPER SKIN DISBONDED. ACCOMPLISHED PERMANENT REPAIR OF DISBONDED UPPER SKIN ON R/W INBD FLAP BONDED PART 113N2324 IAW B757 57-53
- [SDR FDEA202306141034](https://openairdocs.org/sdr/FDEA202306141034), Jun 14, 2023: DOOR. CRACKED. RMLG BODY DOOR IS CRACKED AT THE FWD INBD CORNER OF THE DOOR TANG. REPAIRED RMLG DOOR FWD INBD CORNER OF THE DOOR TANG IAW B757 SRM 52-80-02-2R FIG 201 SHEET 6,
- [SDR FDEA202306141033](https://openairdocs.org/sdr/FDEA202306141033), Jun 14, 2023: PANEL. DAMAGED. MAIN CABIN - FLOOR PANEL IS SATURATED WITH HYDRAULIC FLUID AT STA 560 TO STA680 LBL24 TO LBL45. REMOVED AND REPLACED FLOOR PANEL AT STA 560 - 680 LBL 24 - LBL45
- [SDR FDEA202306141032](https://openairdocs.org/sdr/FDEA202306141032), Jun 14, 2023: PANEL. DAMAGED. MAIN CABIN - FLOOR PANEL IS SATURATED WITH HYDRAULIC FLUID AT STA 560 TO STA680 LBL 0 TO LBL 24. REMOVED AND REPLACED FLOOR PANEL AT STA 560-680 LBL 0 - LBL 24 
- [SDR FDEA202209212353](https://openairdocs.org/sdr/FDEA202209212353), Sep 21, 2022: CASE. CORRODED. #2 ENGINE LPC CASE HAS EVIDENCE OF CORROSION UNDER THE KEVLAR CONTAINMENT RING OUTER SLEEVE AT THE REAR EDGE FROM APPROX 7:00 POSITION TO THE APPROX 12:00 POSIT
- [SDR FDEA202208252049](https://openairdocs.org/sdr/FDEA202208252049), Aug 25, 2022: GIRT BAR. UNSECURE. FOUND L1 DOOR GIRT BAR LAYING ON CREW STAIRS. FACT 24AUG22 18:26 BNA REINSTALLED L1 DOOR GIRT BAR ASSY. PER AMM 25-66-10-2, ALL OPS CKS GOOD PER AMM 52-11-25-5.
- [SDR FDEA202202020179](https://openairdocs.org/sdr/FDEA202202020179), Feb 2, 2022: OIL SYSTEM. OVERSERVICED. SUSPECTED FUME EVENT. STRONG DIRTY SOCK SMELL DESCENDING THROUGH 10,000 FT. WHICH LASTED APPROXIMATELY 3 MINUTES. REMOVED HEPA FILTER PERFOMED GVI IT WAS CLEAN 
- [SDR FDEA2022020320179](https://openairdocs.org/sdr/FDEA2022020320179), Feb 2, 2022: UNKNOWN. FUMES. SUSPECTED FUME EVENT. STRONG DIRTY SOCK SMELL DESCENDING THROUGH 10,000 FT. WHICH LASTED APPROXIMATELY 3 MINUTES.
- [SDR FDEA202109162317](https://openairdocs.org/sdr/FDEA202109162317), Sep 16, 2021: ANNUNCIATOR. FAILED. PDIS 934 32-60 1456 16SEP21 MEM OPEN U ON FINAL 36R KMEM AT 1300 AGL 150 KIAS WITH GEAR LEVER - DOWN RIGHT MAIN NO INDICATION, LEFT MAIN AND NOSE GEAR- DOWN/ GR
- [SDR FDEA202107271877](https://openairdocs.org/sdr/FDEA202107271877), Jul 27, 2021: DOME NUT. CORRODED. DAMAGED AND CORRODED DOME NUT PLATES UNDER FLOOR PANEL 242MGF REMOVED DAMAGED CROWN SUPPORT IAW SRM 51-40-02, FABED NEW CROWN SUPPORT IAW BOEING DWG 111N5207 AN
- [SDR FDEA202107151790](https://openairdocs.org/sdr/FDEA202107151790), Jul 15, 2021: FLOOR PANEL. DAMAGED. ZONE 220 FLOOR BOARD 221AF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221AF ON VTMAE TRAVELER # T21/1560980 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202107151789](https://openairdocs.org/sdr/FDEA202107151789), Jul 15, 2021: FLOOR PANEL. DAMAGED. ZONE 220 FLOOR BOARD 221BF IS BROKEN. FABRICATED ZONE 220 FLOOR BOARD 221BF ON VTMAE TRAVELER # T21/1561021 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202107151788](https://openairdocs.org/sdr/FDEA202107151788), Jul 15, 2021: FLOOR PANEL. DAMAGED. ZONE 220 FLOOR BOARD 222MAF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MAF ON VTMAE TRAVELER # T21/1560977 IAW DWG SRZ- 25-005 REVISION R, MAJOR REPAIR.
- [SDR FDEA202107141775](https://openairdocs.org/sdr/FDEA202107141775), Jul 14, 2021: FLOORBOARD. DELAMINATED. ZONE 200 FLOOR BOARD 222MDF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 222MDF ON VT MAE TRAVELER # T21/1560978 IAW DWG SRZ-25-005 REV R. MAJOR REPAIR.
- [SDR FDEA202107141776](https://openairdocs.org/sdr/FDEA202107141776), Jul 14, 2021: FLOORBOARD. DELAMINATED. ZONE 220 FLOOR BOARD 221MBF IS DAMAGED. FABRICATED ZONE 220 FLOOR BOARD 221MBF ON VT MAE TRAVELERE # T21/1560979 IAW DWG SRZ-25- 005 REV R. MAJOR REPAIR
- [SDR FDEA202103300801](https://openairdocs.org/sdr/FDEA202103300801), Mar 30, 2021: ADC. FAILED. DECLARED EMERGENCY WITH ATC. LIGHTNING STRIKE, UNRELIABLE AIRSPEED ON CAPT/LEFT SIDE. RAN UNRELIABLE AIRSPEED QRH. LANDED FLAPS 20 REF20.RECEIVED MULTIPLE RANDO
- [SDR FDEA202102030299](https://openairdocs.org/sdr/FDEA202102030299), Feb 3, 2021: GIRT BAR. DAMAGED. GIRT BAR NEEDED REPAIR. PIECE FELL OFF DURING CLOSURE ON L1 DOOR. RMV & INSTALL NEW L1 DOOR GIRT BAR IF PLACE REF B757 AMM 25-66-10-2. STILL REQ 52-11-25 25-5 N
- [SDR FDEA202102030275](https://openairdocs.org/sdr/FDEA202102030275), Feb 3, 2021: GIRT BAR. NO TEST. L-1 DOOR FAILED STEP 3 OF E.O. F-5220-7-5000 REV NO. B PS PT3 REF 757 AMM 52-11-20-5, WHILE PERFORMING STEP 3. E.(2), WHEN OUTSIDE HANDLE IS EXTENDED (WITH MODE
- [SDR FDEA202010302721](https://openairdocs.org/sdr/FDEA202010302721), Oct 30, 2020: CONTROL UNIT. WORN. EXCESSIVE ELEVATOR PLAY, FIRST FEW INCHES OF ELEVATOR YOLK INPUT, A DEAD SPOT WAS NOTED, WHERE THERE WAS VERY LITTLE RESISTANCE OR FEEL. VERY NOTEABLE DURING TO
- [SDR FDEA201907031471](https://openairdocs.org/sdr/FDEA201907031471), Jul 3, 2019: FLOORBEAM. CRACKED. CRACK STA. 580 FLOORBEAM LBL 45.50 UPPER CHORD AFT FLANGE. DOT 88-42 COMPLIED WITH EA # : F-5310-T0347950 P1 TITLE: FUSELAGE- MAINFRAME- STA 580 FLOORBEAM SPLIC

All 539: https://openairdocs.org/aircraft/N934FD/reports.md

## STCs that may be installed (OpenAirDocs) (1)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the engine (Rolls-Royce RB211-535E4 series)

- [STC SA4005NM](https://openairdocs.org/stc/SA4005NM): Precise Flight Inc. Pulselite Control System. Precise Flight Inc. Lists RB211-535E4-37

## Related

- Other Boeing 757-21B aircraft: https://openairdocs.org/model/boeing-757-21b/aircraft.md
- The Rolls-Royce RB211-535E4 series engine: https://openairdocs.org/engine/rolls-royce-rb211-535e4-series.md

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